EP1268164B1 - Component consisting of a fibre-reinforced synthetic material and a method for producing same - Google Patents
Component consisting of a fibre-reinforced synthetic material and a method for producing same Download PDFInfo
- Publication number
- EP1268164B1 EP1268164B1 EP01955094A EP01955094A EP1268164B1 EP 1268164 B1 EP1268164 B1 EP 1268164B1 EP 01955094 A EP01955094 A EP 01955094A EP 01955094 A EP01955094 A EP 01955094A EP 1268164 B1 EP1268164 B1 EP 1268164B1
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- EP
- European Patent Office
- Prior art keywords
- winding
- component
- wound
- intermediate structure
- semi
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
- B62D29/04—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of synthetic material
- B62D29/041—Understructures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/564—Winding and joining, e.g. winding spirally for making non-tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
Definitions
- the invention relates to a component made of fiber-reinforced plastic according to the preamble of Claim 1.
- the invention further relates to a method for producing a fiber-reinforced plastic wound component, such as a carrier or a rim.
- Fiber-reinforced plastics are increasingly used in the manufacture of components in Lightweight construction.
- the fiber materials and the low weight of the components are especially important in vehicle construction for the production of body parts, in the construction of rail vehicles for passenger cells, but also used in aircraft construction.
- injection processes resin transfer molding
- fiber winding processes used.
- the fiber winding process is one of the first manufacturing processes for the processing of Composites were developed.
- the advantage of the method is that the fibers in one continuous process can be wound on a mandrel.
- the fibers are often in the impregnated with a resin and wet impregnated in the same operation.
- the fiber winding process is characterized by a high laminate quality and a high accuracy in the fiber resin content and in fiber orientation with a high degree of automation and high economic efficiency out.
- cover caps for rotors and the like the fiber winding process also comes for the production of cover layers used, for example, in the case of passenger compartments around a large rectangular hollow core is wound from rigid foam.
- load-bearing components for example beams in machine and vehicle construction
- load-bearing components for example beams in machine and vehicle construction
- they are still mainly conventional Materials such as steel, aluminum or titanium for use. These are poured in Forms pressed or machined from solid.
- Such components are also made Thermoplastics known, but also either cast or pressed into molds.
- the object of the present invention is to remedy these disadvantages of the prior art.
- Components are to be created from fiber-reinforced plastics, in particular as load-bearing components can be used in mechanical engineering and vehicle construction. It's supposed to be a construction be created for such components, which can be used flexibly and a defined design of the components.
- a process is to be created that enables such to design and manufacture load-bearing components in accordance with the specific requirements.
- the procedure should be automatable and enable reproducible results to a high degree.
- the components made in this way from a fiber-reinforced plastic are said to have high strength properties have a low weight and be inexpensive to manufacture.
- a semi-finished fiber product impregnated with synthetic resin is preferably in several layers, with preferably directed fibers around one Winding core wound.
- the component is designed as a load-bearing element and includes wound Outer belt parts, which are connected to each other by a half-timbered intermediate structure are.
- the cavities between the outer belt parts and the intermediate structure are at least Filled with a filling material.
- the truss-like support structure gives the possibility to calculate the load-bearing behavior.
- the reverse process takes place by an expected or predetermined load based on the required structure, the winding course and the winding density becomes.
- the truss-like component is then produced as a function of the determined one Values through the well-known fiber winding process, the voids between the Outer belt parts and the intermediate structure are at least partially filled with a filler filled.
- the filling material supports the sections of the lattice-like intermediate structure that are subjected to pressure and prevents an uncontrolled buckling of the same when the Load for which they are designed.
- the load-bearing components produced in this way have, for example, opposite beams Steel have a decisive weight advantage and are always compared to aluminum supports even easier by a factor of 1.5 - 2.
- the wound from preferably directed semi-finished fiber Beam has a tensile strength 1.5 - 2 times higher than a high-strength steel beam.
- the filling material in the cavities of the component in the event of a crash as an energy absorber.
- filling materials come physically or chemically foamed plastics, which meet the requirements Have temperature resistance and / or are flame retardant.
- Alternatively or a metal or ceramic foam can also be used in combination with the plastic foams Filling material can be used.
- the components wound from fiber-reinforced plastic have the advantage of being suitable for all weather conditions and can therefore be used all year round without restrictions.
- the wound support structure can be overmolded conventionally. This allows you to Easiest way to combine surface protection and A class surface quality.
- the temperature resistance the plastic used can be designed according to the area of application. For economic For reasons, a temperature resistance of up to about 180 ° C seems sufficient.
- the inventive load-bearing components are suitable, for example, for use as supports or stiffening elements in lightweight vehicles, for example in the category up to approx. 800 kg. In this category, collision partners are in a phase ratio of about 1: 2 to expected about 1: 3.
- inventive load-bearing components are not only limited to the specified purpose. Your relative simple construction and the design of their strength properties also allows use as a carrier for trucks or in general for transport vehicles without further restrictions to.
- the load-bearing components made of fiber-reinforced plastic are also from environmental aspects advantageous. After the life of a vehicle, for example, simply processed into granules, which can then be used in other applications, for example can be used as a filler. Their disposal is also relatively easy, that the entire construction contains no environmentally hazardous substances.
- the component To improve the load-bearing capacity of the component, it is additionally compressed. This happens for example, in the case of wound components that are filled with foamable filling material during the drying and foaming of the filling material within a closed Shape.
- the winding core is heated for this purpose. This triggers the foaming reaction which in the closed form can generate a relatively large pressure, which causes it to the compression of the component comes.
- the outer belt parts and the truss-like intermediate structure are integrally wound from a quasi-endless semi-finished fiber. While it is principally it is possible to wind the outer belt parts and the intermediate structure separately and afterwards Putting them together, for example gluing them together, is for manufacturing reasons an integral production of the elements in one work step is an advantage. It will practically endless fiber semifinished product on the winding core according to a predetermined sequence wound. In this way, the outer belt parts and the intermediate structure in the manufactured in the same operation. Subsequent joining of the elements is not necessary since they are integral are manufactured together and are practically available as a single component. The integral manufacture has a significant influence on the rigidity of the component.
- the method used for the production of the component according to the invention is a fiber winding method, in particular a fiber winding process. It proves to be firm of the component is advantageous if the semi-finished fiber as a synthetic resin impregnated roving of about 1.5 mm to about 4 mm, preferably about 2.5 mm, thickness is present.
- the semi-finished fiber does not necessarily have to contain only one type of fiber.
- the semi-finished fiber is a combination of different types Fiber structures, for example carbon, aramid or glass fibers, preferably with the same type aligned fiber arrangement.
- the resin matrix of the fiber-reinforced plastic can be thermosetting or thermoplastic Base based. The decision about this depends on qualitative and quantitative requirements to the component.
- the winding core for the production of the structural component according to the invention comprises a number of winding spools that are detachably mounted on a winding plate for the winding process.
- the Winding spools can be in the form of lost parts or even after the wound winding has been completed Removable component and be reusable for the production of other components.
- connection devices for example with threaded holes, equipped for connecting additional components.
- the synthetic resin-impregnated fiber semi-finished product is unidirectional for as long as possible before it is deflected is led.
- the windings are impregnated with synthetic resin Semi-finished fiber therefore always has at least in the framework-like intermediate structure led two adjacent winding coils before changing its winding direction.
- the fiber winding process there is the cross winding process, in which the fiber rovings are each crossed on a winding core be wrapped. In polar winding technology, the rovings are each over the poles of a winding core wound. These techniques are used in particular in connection with losing cores Application.
- the strength of the structural component according to the invention made of fiber-reinforced Plastic proves to be of advantage if the synthetic resin-impregnated fiber semi-finished product essentially parallel webs are present side by side and / or wound one above the other.
- the outer belt parts and the intermediate structure are usually not wound homogeneously.
- Much more the component designed according to the invention offers the possibility of individual areas of the Outer belt parts and the lattice-like intermediate structure depending on requirements with a different Number of windings to be provided.
- the load-bearing component can be specific requirements will be strengthened accordingly in individual areas while other sections of the component are provided with targeted weakenings.
- the structure the framework can be symmetrical as well as asymmetrical. In case of use As a carrier in a vehicle chassis, crumplings and crates can be calculated very precisely in this way Compression zones can be created.
- the outer belt parts each comprise a wound upper belt and one coiled lower chord, which through the integral, half-timbered intermediate structure with each other are connected.
- This relatively simple, truss-like design of the support allows good predictability of its properties.
- the upper and lower chords are connected by two coiled side straps connected.
- the side straps also form a cover for the intermediate structure. This prevents foreign bodies from entering the intermediate structure and may also be desirable for aesthetic reasons.
- the side straps are included Advantage wrapped integrally with the top and bottom straps and the intermediate structure. To this Formed in this way, the entire load-bearing component is present as an integral individual body.
- the outer belt parts are arranged in a circle and form an inside essentially annular outer surface.
- the wound component is a rim.
- the Composite rim has a sufficiently high strength. It is much lighter than comparable ones Rims of conventional steel construction. Even compared to aluminum rims, the Composite rim weight advantages.
- the circular arrangement of the outer belt parts through a half-timbered intermediate structure is connected to each other, also allows the production other rotationally symmetrical components, for example gripper wheels, used for manufacturing of tapes, belts and the like are used.
- the component can be designed to be largely closed Outer skin to be provided, the penetration and deposition of contaminants prevented inside the component.
- the semi-finished fiber in a winding process, preferably straightened, wound on a winding core and then cured and dried.
- the process draws is characterized in particular by the fact that in the winding of the semi-finished fiber an arrangement of Winding spools created a number of outer belt parts and integrally with a winding technology truss-like intermediate structure can be wound.
- the upper and lower chord and the truss-like intermediate structure of the wound component integrally, in the same operation from a quasi-infinite semi-finished fiber wound.
- the outer belt parts lie the intermediate structure connecting them as a single element in front.
- the voids between the outer belt parts and the intermediate structure are at least partially filled with a filling material.
- the constructive design and the filling The cavities increase the overall strength of the component and facilitate the manufacturing process. Due to the integral winding process, the component is very simple, according to the requirements, can be laid out and wound.
- the filling material supports the sections of the truss-like sections that are subjected to pressure Intermediate structure and prevents an uncontrolled buckling of the same when exceeded the load for which they are designed.
- the filling material can include the energy intake favor in the event of a crash and an uncontrolled buckling of those under pressure Prevent branches of the truss-like intermediate structure.
- a filler for example we chose a technical plastic foam that is physically or chemically foamable.
- a metal or ceramic foam can also be used as a filling material in the Spaces are introduced.
- the method according to the invention for producing fiber-reinforced components makes it possible to the number of windings created one above the other and / or next to one another and the course of the windings over the coils arranged side by side and one behind the other depending on the to select the forces to be absorbed by the wound component. This allows the component to be specific be designed for the planned load.
- the structural design of the component according to the type of truss enables a relatively simple calculation of the component and the specific one Interpretation.
- the winding coils can be removed from the component after the winding process in order for them continue to use the manufacture of additional components. It is also possible to provide individual winding coils, which were designed as inserts and with connection devices, for example threaded holes, were equipped for the attachment of further connection components, such as in the integrated component that they form an integral part of the component.
- the semifinished fiber product becomes during the winding process in the framework-like Intermediate structure in each case via at least two winding coils arranged next to one another of the winding core before the longitudinal alignment of the fibers by changing the Winding direction is changed.
- a parallel winding process has proven to be advantageous for the strength of the load-bearing component which the semifinished fiber product in essentially parallel windings over the individual winding coils is wound.
- Crossings of the windings come on the winding spools practically only with superimposed winding layers.
- the method according to the invention can be carried out manually, semi-automatically or fully automatically become.
- the method according to the invention is particularly suitable for CNC path-controlled Winding machines, which offer the possibility of changing the fiber layer, the winding pattern, the thread tension, the stoichiometric ratio of fibers to the resin matrix, etc. microprocessor controlled to control and regulate.
- the determined load values can be directly converted into design data and be used for the control and regulation of the winding machine.
- carbonized natural fibers are advantageously used as semi-finished products made of flax, hemp or Chinese reed or carbon, aramid and / or e-glass rovings Application that is done beforehand or just before the winding process in an impregnation device with a thermosetting or thermoplastic matrix of a two-component resin be soaked.
- the thickness of the impregnated roving is preferably about 1.5 mm to about 4 mm about 2.5 mm.
- the field of application of the wound, load-bearing components according to the invention extends from use in vehicle construction to mechanical engineering applications, civil engineering to to space applications. Applications can be found wherever lightweight construction is required or is desired. Vehicle construction is highlighted as a special area of application, where the construction of the components according to the invention and the manufacturing process simple design of the components for use as crash elements in chassis construction.
- the component in the In the case of beams, the component is wrapped with a top and a bottom flange manufactured by an integrally wound, truss-like intermediate structure connected to a unit.
- one is used for winding Number of outer belt parts made, which are arranged in a circle. They switch on Circumference with large winding spools.
- the semi-finished fiber-impregnated resin is thereby before and after winding an outer belt part each over a large winding spool.
- the semi-finished fiber is between the winding over two large winding coils arranged on the circumference each led through a section of the truss-like intermediate structure.
- Fig. 1 shows schematically a process known as bulk fiber winding method, which is preferably for Production of the components according to the invention from fiber-reinforced plastic is used.
- a semi-finished fiber P held by a tensioning unit 2 is pretensioned by one Supply spool 1 is removed and passed through an impregnation unit 3.
- the impregnation unit 3 can as a dip impregnation device or, as shown for example, as a roller impregnation device be trained.
- the various forms of impregnation units are sufficient for the person skilled in the art known, so that a further explanation can be omitted.
- the semi-finished fiber includes, for example, directional carbon, aramid or glass fibers as individual fibers or, as required, in any combination with each other and is a roving with a thickness of about 1.5 mm to about 4 mm, preferably 2.5 mm, before. Carbonized natural fibers from flax, hemp or Chinese reed can also be used become.
- the synthetic resin is advantageously a thermoplastic or thermosetting two-component resin,
- FIG. 2 shows an example of a winding system 10, in particular a computer-controlled CNC winding system.
- This comprises a winding machine 11, a machine controller 12 and one Machine computer 13.
- the interaction of the individual system components is with each other illustrated by the double arrows 14 and 15.
- the machine computer 13 is used for real-time control of the machine and for real-time management of the control data in control mode. He allows programming, management and graphical representation of the control data in program mode.
- the control data for example the Optimize the speed of the winding core.
- the machine controller 12 of the winding system 10 is responsible for regulation, control and communication.
- the Machine control also controls other relevant process parameters, for example the thread tension of the semi-finished fiber.
- the communication function enables one Data exchange between the winding machine 11 and the machine computer 13.
- the winding machine 10 is preferred as a rotary winding machine with an axis of rotation for the winding head, a slide adjustable in the plane and an infeed axis.
- the elements of the Winding machine have the required number of degrees of freedom of movement, thus components of the desired type can be wound. For the production of somewhat more complex components are preferred six degrees of freedom are provided.
- FIG. 3 shows an initial situation for the production of a component according to the invention.
- winding coils there is a number of winding coils, numbered 21-30, next to and below mounted one behind the other on a winding plate 20.
- the winding plate 20 forms a component of the winding core 5 (Fig. 1).
- the winding spools 21-30 can be made of metal or plastic his.
- the impregnated semi-finished fiber P drawn off as roving from the supply reel becomes deposited on the winding spools 21-30 according to a predetermined winding plan.
- the winding plan depends on the control data stored in the machine computer, which is preferably dependent was determined from the expected load on the component to be manufactured.
- Such a winding plan can, for example, by specifying the one to be started Winding spools are set.
- a winding plan could do the following Show course: S; 21; 23; 26; 28; 29; 30; 29; 30; 28; 25; 23; 22; 21; 22; 21; 24; 26; 27; 29; 30; 27; 25; 24; 22; 21; 23; 25; 27; 29; 30; 28; 26; 24; 22; 21; etc.; E.
- S denote the beginning of the stored roving P, the reference symbols the winding coils which follow one another in the winding direction and E the end of the roving P.
- the winding plan given serves only to explain the Winding process and therefore does not represent a mandatory scheme. Rather, it depends on the one to be created Component geometry to define a new winding plan. It should be borne in mind that The roving is guided for as long as possible before being loaded the winding direction and thus the direction of the fibers is changed.
- Fig. 4 shows the apparatus structure for a further advantageous process step in the manufacture of a load-bearing component made of fiber-reinforced plastic according to the invention. That done
- the wound component is provided with the reference symbol 40 as a whole.
- some of the winding coils 21-30 can be designed as lost parts. These remain in the wound component and form an integral part.
- they can be designed as inserts 21, 22, 29, 30, with threaded bores 35 for connecting further Components on the component 40 are equipped.
- the remaining winding spools 23 - 28 can be from Component 40 can be removed in order to use them further for the production of further wound components.
- the finished wound component 40 is still arranged on the winding plate 20 in FIG. 4.
- the closing form 31 is supported on the winding plate 20 and can be closed by a cover 32.
- the lid is with holes and closable filler openings 33 through which a filler material into the wound component 40 remaining cavities can be filled.
- the filler a physically or chemically foamable engineering plastic or a metal or ceramic foam used. Due to the expansion of the filling material while the component is drying 40 in the closed closing form 31, the windings are compressed. Thereby the strength of the wound component 40 is increased still further. After compression, it will Component 40 annealed in the closing mold or after it has been removed from the mold.
- Component comprises an upper chord 41 and a lower chord 42, which are constructed by a framework Intermediate structure 43 are integrally connected to one another. It has on its longitudinal ends Component 40 each have a side belt 44, 45 which is also integral with the upper and lower belts 41, 42 and the truss-like intermediate structure 43 is wound. Integrated in the side straps 44, 45 are the inserts 21, 22 and 29, 30, each with threaded holes 35 for connecting further Structural elements are equipped. That is the spaces between the upper and lower chords 42, 42 and the intermediate structure 43 filling, foamed filler is with the reference numeral 46 provided. For the purpose of illustration, the foamed packing elements 46 are of different widths shown inserted.
- the wall thicknesses of the upper and lower chords 41, 42, the side chords 44, 45 and the truss-like intermediate structure 43 can, depending on the expected load on the Component, according to the calculated design to be different in some areas. This can be achieved by a different winding density.
- the component can fiber-reinforced plastic can be tailored with regard to its later use. For example weakened areas can be built in in order to use the component to realize a crumple zone in a vehicle chassis.
- the component 40 can also have an outer skin, for example a sprayed-on one Be plastic skin. To be used in extremely adverse physical environmental conditions or to ensure chemical origin, the wound support structure can be overmolded conventionally become. This allows surface protection and A class surface quality in the simplest way combine.
- the winding component indicated in FIG. 6 is essentially rotationally symmetrical and bears the reference number 50 in its entirety.
- the illustration shows a ring-shaped arrangement Profile in which large winding spools 57-61 arranged on the circumference with outer belt parts 62-66 alternate.
- the outer belt parts 62-66 are preferably curved in the manner of a segment of a circle Outside molded parts wrapped.
- the truss-like intermediate structure has winding coils 51-56.
- the winding sequence can, for example, have the following course: from the one in the center Winding spool 51 becomes the semi-finished fiber P, for example an impregnated fabric tape, to the winding spool 52 and from there to the large winding spool 57 located on the circumference.
- the large winding spool 57 is preferably wrapped before the fabric tape P to the segment of a circle curved outer molded part to form the outer belt part 62 is passed this is wound and passed to the next large winding spool 61.
- the fabric tape P is again guided into the framework-like intermediate structure, where it is first unidirectionally over the winding coils 56 and 51 before its Winding direction is changed in the direction of the winding spool 54. Arrived from the winding spool 54 the fabric tape P to large winding spool 59 arranged on the circumference. This is preferred at least once rounds before the fabric tape P on the outer molded part for the outer belt part 64 is directed.
- the belt P is around the adjacent large winding spool 58 out before it again to the winding spools in the framework Intermediate structure is passed, etc. This ensures that the fabric tape always led alternately over a section of the circumference and the intermediate structure becomes.
- the fabric tape P is always over two large winding spools and one in between arranged outer belt part guided.
- the fabric tape is always first passed over two adjacent winding coils before changing its winding direction.
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Abstract
Description
Die Erfindung betrifft ein Bauteil aus faserverstärktem Kunststoff gemäss dem Oberbegriff des Patentanspruchs 1. Die Erfindung betrifft weiters aucb ein Verfahren zur Herstellung eines aus faserverstärktem Kunststoff gewickelten Bauteils, beispielsweise eines Trägers oder einer Felge.The invention relates to a component made of fiber-reinforced plastic according to the preamble of Claim 1. The invention further relates to a method for producing a fiber-reinforced plastic wound component, such as a carrier or a rim.
Faserverstärkte Kunststoffe finden zunehmend Verbreitung in der Herstellung von Bauteilen in Leichtbauweise. Durch die Fortschritte in der Materialentwicklung im Bereich der Kunststoffe und der Fasermaterialien und das geringe Gewicht der Bauteile werden diese vor allem auch im Fahrzeugbau für die Herstellung von Karosserieteilen, im Bau von Schienenfahrzeugen für Fahrgastzellen, aber auch im Flugzeugbau verwendet. Je nach Art des Bauteils werden zur Herstellung der Bauteile Laminiertechniken, Injektionsverfahren (Resin Transfer Moulding) oder Faserwickelverfahren eingesetzt.Fiber-reinforced plastics are increasingly used in the manufacture of components in Lightweight construction. By advances in material development in the field of plastics and The fiber materials and the low weight of the components are especially important in vehicle construction for the production of body parts, in the construction of rail vehicles for passenger cells, but also used in aircraft construction. Depending on the type of component used to manufacture the Components laminating techniques, injection processes (resin transfer molding) or fiber winding processes used.
Das Faserwickelverfahren zählt zu den ersten Herstellungsverfahren, die für die Verarbeitung von Composites entwickelt wurden. Der Vorteil des Verfahrens liegt darin, das die Fasern in einem kontinuierlichen Prozess auf einen Formkern gewickelt werden. Dabei werden die Fasern häufig im selben Arbeitsgang mit einem Harz durchtränkt und nass imprägniert. Das Faserwickelverfahren zeichnet sich durch eine hohe Laminatqualität und eine hohe Genauigkeit im Faserharzgehalt und in der Faserorientierung bei gleichzeitig hohem Automatisierungsgrad und hoher Wirtschaftlichkeit aus. Neben der Herstellung kleinerer Spezialbauteile, beispielsweise von Abdeckkappen für Rotoren und dergleichen, kommt das Faserwickelverfahren auch für die Herstellung von Deckschichten zum Einsatz, die beispielsweise im Fall von Fahrgastzellen um einen grossen rechteckigen Hohlkern aus Hartschaumstoff gewickelt wird.The fiber winding process is one of the first manufacturing processes for the processing of Composites were developed. The advantage of the method is that the fibers in one continuous process can be wound on a mandrel. The fibers are often in the impregnated with a resin and wet impregnated in the same operation. The fiber winding process is characterized by a high laminate quality and a high accuracy in the fiber resin content and in fiber orientation with a high degree of automation and high economic efficiency out. In addition to the manufacture of smaller special components, such as cover caps for rotors and the like, the fiber winding process also comes for the production of cover layers used, for example, in the case of passenger compartments around a large rectangular hollow core is wound from rigid foam.
Für die Herstellung von tragenden Bauteilen, beispielsweise von Trägern im Maschinen- und Fahrzeugbau, kommen trotz der bekannten Vorteile der Composites immer noch hauptsächlich konventionelle Werkstoffe, wie Stahl, Aluminium oder Titan zur Verwendung. Diese werden gegossen, in Formen gepresst oder aus dem Vollen spanabhebend bearbeitet. Es sind auch derartige Bauteile aus Thermoplasten bekannt, die aber gleichfalls entweder gegossen oder in Formen gepresst werden. For the production of load-bearing components, for example beams in machine and vehicle construction, despite the well-known advantages of composites, they are still mainly conventional Materials such as steel, aluminum or titanium for use. These are poured in Forms pressed or machined from solid. Such components are also made Thermoplastics known, but also either cast or pressed into molds.
Die bekannten Materialien für die Herstellung von tragenden Bauteilen weisen alle entweder ein hohes Gewicht auf oder sie sind aufwendig und teuer in der Herstellung und der Verarbeitung. Der Einsatz von Kunststoffverbundmaterialien bei der Herstellung von Fahrzeugen in Leichtbauweise führte bislang nicht zu den gewünschten Ergebnissen. Insbesondere im Crash-Verhalten weisen die bekannten Kunststoffbauweisen nur ungenügende Resultate auf, weshalb sie im allgemeinen durch vergleichsweise schwere Metallkonstruktionen für die crash-relevanten, tragenden Bauteile ergänzt werden.The known materials for the production of load-bearing components all have either heavy weight or they are complex and expensive to manufacture and process. The Use of plastic composite materials in the manufacture of lightweight vehicles has so far not led to the desired results. Especially when it comes to crash behavior known plastic designs only insufficient results, which is why they generally by comparatively heavy metal structures for the crash-relevant, load-bearing components added become.
Aufgabe der vorliegenden Erfindung ist es, diesen Nachteilen des Stands der Technik abzuhelfen. Es sollen Bauteile aus faserverstärkten Kunststoffen geschaffen werden, die insbesondere auch als tragende Bauteile im Maschinenbau und im Fahrzeugbau einsetzbar sind. Es soll eine Konstruktion für derartige Bauteile geschaffen werden, die flexibel einsetzbar ist und eine definierte Auslegung der Bauteile ermöglicht. Dazu soll ein Verfahren geschaffen werden, dass es ermöglicht, derartige tragende Bauteile gemäss den spezifischen Anforderungen auszulegen und herzustellen. Das Verfahren soll automatisierbar sein und in einem hohen Mass reproduzierbare Ergebnisse ermöglichen. Die derart hergestellten Bauteile aus einem faserverstärkten Kunststoff sollen bei hohen Festigkeitseigenschaften ein geringes Gewicht aufweisen und kostengünstig in der Herstellung sein.The object of the present invention is to remedy these disadvantages of the prior art. Components are to be created from fiber-reinforced plastics, in particular as load-bearing components can be used in mechanical engineering and vehicle construction. It's supposed to be a construction be created for such components, which can be used flexibly and a defined design of the components. For this purpose, a process is to be created that enables such to design and manufacture load-bearing components in accordance with the specific requirements. The procedure should be automatable and enable reproducible results to a high degree. The components made in this way from a fiber-reinforced plastic are said to have high strength properties have a low weight and be inexpensive to manufacture.
Die Lösung dieser Aufgaben besteht in einem Bauteil aus faserverstärktem Kunststoff mit den im kennzeichnenden Abschnitt des Patentanspruchs 1 angeführten Merkmalen. Vorteilhafte Weiterbildungen und/oder Varianten der Erfindung sind Gegenstand der abhängigen Vorrichtungsansprüche. Das erfindungsgemässe Verfahren zeichnet sich insbesondere durch die im kennzeichnenden Abschnitt des unabhängigen Verfahrensanspruchs angeführten Schritte aus. Vorteilhafte Weiterbildungen und/oder Varianten der Verfahrensführung sind Gegenstand der abhängigen Verfahrensansprüche.The solution to these tasks consists in a component made of fiber-reinforced plastic with the im characterizing section of claim 1. Advantageous further training and / or variants of the invention are the subject of the dependent device claims. The method according to the invention is characterized in particular by that in the characterizing section of the independent procedural claim. Advantageous further training and / or variants of the procedure are the subject of the dependent claims.
Bei einem Bauteil aus faserverstärktem Kunststoff ist ein kunstharzharzimprägniertes Fascrhalbzeug, vorzugsweise in mehreren Schichten, mit vorzugsweise direktionierten Fasern um einen Wickelkern gewickelt. Das Bauteil ist als tragendes Element ausgebildet und umfasst gewickelte Aussengurtteile, die durch eine fachwerkartig gewickelte Zwischenstruktur miteinander verbunden sind. Die Hohlräume zwischen den Aussengurtteilen und der Zwischenstruktur sind wenigstens bercichsweise mit einem Füllmaterial ausgefüllt. In the case of a component made of fiber-reinforced plastic, a semi-finished fiber product impregnated with synthetic resin is preferably in several layers, with preferably directed fibers around one Winding core wound. The component is designed as a load-bearing element and includes wound Outer belt parts, which are connected to each other by a half-timbered intermediate structure are. The cavities between the outer belt parts and the intermediate structure are at least Filled with a filling material.
Durch die erfindungsgemässe Ausbildung des tragenden Bauteils ist dieses relativ einfach auslegbar. Im Gegensatz zu den bisherigen, gegossenen oder in Formen gepressten Bauteilen, bietet die fachwerkartig gewickelte Trägerstruktur die Möglichkeit, das Tragverhalten zu berechnen. In der Praxis erfolgt der umgekehrte Vorgang, indem von einer zu erwartenden oder vorgegebenen Belastung ausgehend die erforderliche Struktur, der Wickelverlauf und die Wicklungsdichte festgelegt wird. Die Herstellung des fachwerkartigen Bauteils erfolgt sodann in Abhängigkeit von den ermittelten Werten durch das hinlänglich bekannte Faserwickelverfahren, Die Hohlräume zwischen den Aussengurtteilen und der Zwischenstruktur sind wenigstens bereichsweise mit einem Füllmaterial ausgefüllt. Das Füllmaterial stützt die auf Druck belasteten Abschnitte der fachwerkartigen Zwischenstruktur und verhindert ein unkontrolliertes Ausknicken derselben bei Überschreitung der Belastung, für die sie ausgelegt sind.Due to the inventive design of the load-bearing component, it can be designed relatively easily. In contrast to previous, cast or pressed components, the truss-like support structure gives the possibility to calculate the load-bearing behavior. In the In practice, the reverse process takes place by an expected or predetermined load based on the required structure, the winding course and the winding density becomes. The truss-like component is then produced as a function of the determined one Values through the well-known fiber winding process, the voids between the Outer belt parts and the intermediate structure are at least partially filled with a filler filled. The filling material supports the sections of the lattice-like intermediate structure that are subjected to pressure and prevents an uncontrolled buckling of the same when the Load for which they are designed.
Die auf diese Weise hergestellten tragenden Bauteile weisen beispielsweise gegenüber Trägern aus Stahl einen entscheidenden Gewichtsvorteil auf und sind auch gegenüber Aluminiumträgem immer noch um einen Faktor 1,5 - 2 leichter. Der aus vorzugsweise gerichtetem Faserhalbzeug gewickelte Träger weist eine um einen Faktor 1,5 - 2 höhere Zugfestigkeit auf als ein hochfester Stahlträger. Bei der Verwendung des Bauteils als Träger in einem Fahrzeugschassis dient das Füllmaterial in den Hohlräumen des Bauteils im Crashfall als Energieabsorber. Als Füllmaterialien kommen physikalisch oder chemisch geschäumte Kunststoffe in Frage, die eine den Anforderungen entsprechende Temperaturbeständigkeit aufweisen und/oder schwer entflammbar sind. Alternativ oder auch in Kombination zu den Kunststoffschäumen kann auch ein Metall- oder Keramikschaum als Füllmaterial eingesetzt werden.The load-bearing components produced in this way have, for example, opposite beams Steel have a decisive weight advantage and are always compared to aluminum supports even easier by a factor of 1.5 - 2. The wound from preferably directed semi-finished fiber Beam has a tensile strength 1.5 - 2 times higher than a high-strength steel beam. When the component is used as a carrier in a vehicle chassis, the filling material in the cavities of the component in the event of a crash as an energy absorber. As filling materials come physically or chemically foamed plastics, which meet the requirements Have temperature resistance and / or are flame retardant. Alternatively or a metal or ceramic foam can also be used in combination with the plastic foams Filling material can be used.
Die aus faserverstärktem Kunststoff gewickelten Bauteile besitzen den Vorteil der Allwettertauglichkeit und können daher, ohne Einschränkungen, das ganze Jahr über eingesetzt werden. Um den Einsatz in extrem widrigen Umwelteinflüssen physischen oder chemischen Ursprungs zu gewährleisten, kann die gewickelte Tragstruktur herkömmlich umspritzt werden. Dadurch lassen sich auf einfachste Weise Oberflächenschutz und A Klasse Oberflächenqualität vereinen. Die Temperaturfestigkeit des verwendeten Kunststoffs ist nach dem Einsatzgebiet auslegbar. Aus wirtschaftlichen Gründen erscheint eine Temperaturbeständigkeit bis etwa 180°C dabei als ausreichend. Die erfindungsgemässen tragenden Bauteile eignen sich beispielsweise für den Einsatz als Träger oder Versteifungselemente in Fahrzeugen in Leichbauweise, beispielsweise in der Kategorie bis ca. 800 kg. In dieser Kategorie sind im Crashfall Stosspartner in einem Masenverhältnis von etwa 1 : 2 bis etwa 1 : 3 zu erwarten. Derartige Fahrzeuge sind hauptsächlich im Nahbereich unterwegs und dadurch einem erhöhten Crashrisiko ausgesetzt. Die aus der Verwendung der erfindungsgemässen tragenden Bauteile als Chassisbauteile erzielbare Gewichtseinsparung erweist sich insbesondere bei dem angegebenen Einsatzgebiet als energetisch besonders günstig. Die erfindungsgemässen tragenden Bauteile sind jedoch nicht nur auf den angegebenen Einsatzzweck beschränkt. Ihre relativ einfache Konstruktion und die Auslegbarkeit ihrer Festigkeitseigenschaften lässt auch den Einsatz als Träger bei Lastkraftfahrzeugen oder generell bei Transportfahrzeugen ohne weitere Einschränkungen zu. Die tragenden Bauteile aus faserverstärktem Kunststoff sind auch aus Umweltaspekten von Vorteil. Sie können nach Ablauf der Lebensdauer, beispielsweise eines Fahrzeugs, einfach zu Granulat weiterverarbeitet werden, welches dann beispielsweise in anderen Anwendungen als Füllstoff eingesetzt werden kann. Ihre Entsorgung ist ebenfalls relativ problemlos, das die gesamte Konstruktion keinerlei umweltgefährdende Stoffe enthält.The components wound from fiber-reinforced plastic have the advantage of being suitable for all weather conditions and can therefore be used all year round without restrictions. To the Ensure use in extremely adverse environmental influences of physical or chemical origin, the wound support structure can be overmolded conventionally. This allows you to Easiest way to combine surface protection and A class surface quality. The temperature resistance the plastic used can be designed according to the area of application. For economic For reasons, a temperature resistance of up to about 180 ° C seems sufficient. The inventive load-bearing components are suitable, for example, for use as supports or stiffening elements in lightweight vehicles, for example in the category up to approx. 800 kg. In this category, collision partners are in a phase ratio of about 1: 2 to expected about 1: 3. Such vehicles are mainly in the vicinity and therefore exposed to an increased risk of crash. The from the use of the inventive load-bearing components as chassis components achievable weight saving proves in particular in the specified area of application as energetically particularly favorable. The inventive load-bearing components are not only limited to the specified purpose. Your relative simple construction and the design of their strength properties also allows use as a carrier for trucks or in general for transport vehicles without further restrictions to. The load-bearing components made of fiber-reinforced plastic are also from environmental aspects advantageous. After the life of a vehicle, for example, simply processed into granules, which can then be used in other applications, for example can be used as a filler. Their disposal is also relatively easy, that the entire construction contains no environmentally hazardous substances.
Zur Verbesserung der Tragfestigkeit des Bauteils ist dieses zusätzlich noch verdichtet. Dies erfolgt beispielsweise bei gewickelten und mit schäumbarem Füllmaterial gefüllten Bauteilen automatisch während des Trocknens und Aufschäumens des Füllmaterials innerhalb einer abgeschlossenen Form. Beispielsweise wird dazu der Wickelkern erhitzt. Dabei wird die Schäumungsreaktion ausgelöst, die in der geschlossenen Form einen relativ grossen Druck erzeugen kann, durch den es zu der Verdichtung des Bauteils kommt.To improve the load-bearing capacity of the component, it is additionally compressed. this happens for example, in the case of wound components that are filled with foamable filling material during the drying and foaming of the filling material within a closed Shape. For example, the winding core is heated for this purpose. This triggers the foaming reaction which in the closed form can generate a relatively large pressure, which causes it to the compression of the component comes.
In einer vorteilhaften Variante der Erfindung sind dic Aussengurtteile und die fachwerkartige Zwischenstruktur integral aus einem quasi-endlosen Faserhalbzeug gewickelt. Während es zwar prinzipiell möglich ist, die Aussengurtteile sowie die Zwischenstruktur separat zu wickeln und danach zusammenzurügen, beispielsweise miteinander zu verkleben, ist aus fertigungstechnischen Gründen eine integrale Herstellung der Elemente in einem Arbeitsschritt von Vorteil. Dabei wird das praktisch endlos vorliegende Faserhalbzeug nach einem vorgegebenen Ablaufschema auf den Wikkelkern gewickelt. Auf diese Weise werden die Aussengurtteile sowie die Zwischenstruktur im selben Arbeitsgang hergestellt. Ein nachträgliches Fügen der Elemente entfällt, da sie ja integral miteinander gefertigt werden und praktisch als ein einzelnes Bauteil vorliegen. Die integrale Herstellung hat massgeblich Einfluss auf die Steifigkeit des Bauteils.In an advantageous variant of the invention, the outer belt parts and the truss-like intermediate structure are integrally wound from a quasi-endless semi-finished fiber. While it is principally it is possible to wind the outer belt parts and the intermediate structure separately and afterwards Putting them together, for example gluing them together, is for manufacturing reasons an integral production of the elements in one work step is an advantage. It will practically endless fiber semifinished product on the winding core according to a predetermined sequence wound. In this way, the outer belt parts and the intermediate structure in the manufactured in the same operation. Subsequent joining of the elements is not necessary since they are integral are manufactured together and are practically available as a single component. The integral manufacture has a significant influence on the rigidity of the component.
Das für die Herstellung des erfindungsgemässen Bauteils eingesetzte Verfahren ist ein Faserwikkelverfahren, insbesondere ein Fasernasswickelverfahren. Dabei erweist es sich für die Festigkeit des Bauteils von Vorteil, wenn das Faserhalbzeug als ein kunstharzimprägnierter Roving von etwa 1,5 mm bis etwa 4 mm, vorzugsweise etwa 2,5 mm, Stärke vorliegt. The method used for the production of the component according to the invention is a fiber winding method, in particular a fiber winding process. It proves to be firm of the component is advantageous if the semi-finished fiber as a synthetic resin impregnated roving of about 1.5 mm to about 4 mm, preferably about 2.5 mm, thickness is present.
Das Faserhalbzeug muss nicht unbedingt nur einen einzigen Fasertyp enthalten. Aus Festigkeitsgründen kann es von Vorteil sein, wenn das Faserhalbzeug eine Kombination verschiedenartiger Faserstrukturen, beispielsweise Carbon-, Aramid- oder Glasfasern, mit vorzugsweise gleichartig ausgerichteter Faseranordnung umfasst.The semi-finished fiber does not necessarily have to contain only one type of fiber. For strength reasons it can be advantageous if the semi-finished fiber is a combination of different types Fiber structures, for example carbon, aramid or glass fibers, preferably with the same type aligned fiber arrangement.
Die Harzmatrix des faserverstärkten Kunststoffs kann auf duroplastischer oder thermoplastischer Basis beruhen. Die Entscheidung darüber ist abhängig von qualitativen und quantitativen Anforderungen an das Bauteil.The resin matrix of the fiber-reinforced plastic can be thermosetting or thermoplastic Base based. The decision about this depends on qualitative and quantitative requirements to the component.
Der Wickelkern für die Herstellung des erfindungsgemässen tragenden Bauteils umfasst eine Anzahl von Wickelspulen, die für den Wickelvorgang lösbar auf einer Wickelplatte montiert sind. Die Wickelspulen können als Verlierteile vorliegen oder auch nach der Fertigstellung des gewickelten Bauteils entnehmbar und für die Herstellung von weiteren Bauteilen wiederverwendbar sein.The winding core for the production of the structural component according to the invention comprises a number of winding spools that are detachably mounted on a winding plate for the winding process. The Winding spools can be in the form of lost parts or even after the wound winding has been completed Removable component and be reusable for the production of other components.
Es erweist sich von Vorteil, wenn einzelne der Wickelspulen als Verlierteile, insbesondere als Inserts ausgebildet sind. Die Inserts sind mit Anschlusseinrichtungen, beispielsweise mit Gewindebohrungen, zum Anschluss weiterer Bauteile ausgestattet.It proves to be advantageous if some of the winding coils are lost parts, in particular as Inserts are formed. The inserts are provided with connection devices, for example with threaded holes, equipped for connecting additional components.
Für die Festigkeit des aus einem faserverstärkten Kunststoff gewickelten Bauteils ist es von Vorteil, wenn das kunstharzimprägnierte Faserhalbzeug vor seiner Umlenkung möglichst lange unidirektional geführt ist. Bei dem erfindungsgemässen Bauteil sind die Wicklungen des kunstharzimprägnierten Faserhalbzeugs deshalb in der fachwerkartigen Zwischenstruktur immer über wenigstens zwei benachbarte Wickelspulen geführt, bevor seine Wickelrichtung ändert.For the strength of the component wound from a fiber-reinforced plastic, it is advantageous if the synthetic resin-impregnated fiber semi-finished product is unidirectional for as long as possible before it is deflected is led. In the component according to the invention, the windings are impregnated with synthetic resin Semi-finished fiber therefore always has at least in the framework-like intermediate structure led two adjacent winding coils before changing its winding direction.
Für das Faserwickelverfahren sind unterschiedliche Wickelarten bekannt. So existiert beispielsweise das Kreuzwickelverfahren, bei dem die Faserrovings jeweils gekreuzt auf einen Wickelkern gewickelt werden. In der Polarwickeltechnik werden die Rovings jeweils über die Pole eines Wikkelkerns gewickelt. Diese Techniken kommen insbesondere in Verbindung mit Verlierkernen zur Anwendung. Für die Festigkeit des erfindungsgemässen tragenden Bauteils aus faserverstärktem Kunststoff erweist es sich von Vorteil, wenn das kunstharzimprägnierten Faserhalbzeug in im wesentlichen parallel verlaufenden Bahnen nebeneinander und/oder übereinander gewickelt vorliegt. Different types of winding are known for the fiber winding process. For example, there is the cross winding process, in which the fiber rovings are each crossed on a winding core be wrapped. In polar winding technology, the rovings are each over the poles of a winding core wound. These techniques are used in particular in connection with losing cores Application. For the strength of the structural component according to the invention made of fiber-reinforced Plastic proves to be of advantage if the synthetic resin-impregnated fiber semi-finished product essentially parallel webs are present side by side and / or wound one above the other.
Die Aussengurtteile und die Zwischenstruktur sind in der Regel nicht homogen gewickelt. Vielmehr bietet das erfindungsgemäss ausgebildetet Bauteil die Möglichkeit, einzelne Bereiche der Aussengurtteile und der fachwerkartigen Zwischenstruktur anforderungsspezifisch mit einer unterschiedlichen Anzahl von Wicklungen zu versehen. Auf diese Weise kann das tragende Bauteil seinen späteren Anforderungen entsprechend in einzelnen Bereichen gezielt verstärkt werden, während andere Abschnitte des Bauteils mit gezielten Schwächungen versehen werden. Der Aufbau des Fachwerkes kann sowohl symmetrisch als auch asymmetrisch erfolgen. Im Fall des Einsatzes als Träger in einem Fahrzeugchassis sind auf diese Weise sehr exakt berechenbare Knautsch- und Stauchungszonen erstellbar.The outer belt parts and the intermediate structure are usually not wound homogeneously. Much more the component designed according to the invention offers the possibility of individual areas of the Outer belt parts and the lattice-like intermediate structure depending on requirements with a different Number of windings to be provided. In this way, the load-bearing component can be specific requirements will be strengthened accordingly in individual areas while other sections of the component are provided with targeted weakenings. The structure the framework can be symmetrical as well as asymmetrical. In case of use As a carrier in a vehicle chassis, crumplings and crates can be calculated very precisely in this way Compression zones can be created.
Bei einem Trägerbauteil umfassen die Aussengurtteile je einen gewickelten Obergurt und einen gewickelten Untergurt, die durch die integral, fachwerkartig gewickelte Zwischenstruktur miteinander verbunden sind. Gerade diese relativ einfache, fachwerkartige Ausbildung des Trägers erlaubt eine gute Berechenbarkeit seiner Eigenschaften.In the case of a carrier component, the outer belt parts each comprise a wound upper belt and one coiled lower chord, which through the integral, half-timbered intermediate structure with each other are connected. This relatively simple, truss-like design of the support allows good predictability of its properties.
In einer Variante des Trägers, die auch quer zur Längserstreckung des Ober- und Untergurtes eine erhöhte Festigkeit aufweist, sind der Ober- und Untergurt durch zwei gewickelte Seitengurte miteinander verbunden. Neben ihrer Versteifungsfunktion bilden die Seitengurte auch eine Abdeckung für die Zwischenstruktur. Dies verhindert ein Eindringen von Fremdkörpern in die Zwischenstruktur und kann auch aus ästhetischen Gründen erwünscht sein. Aus fertigungstechnischen Gründen und der besseren Einbindung der Seitengurte in die Gesamtstruktur wegen sind die Seitengurte mit Vorteil integral mit den Ober- und Untergurten und der Zwischenstruktur gewickelt. Auf diese Weise ausgebildet, liegt das gesamte tragende Bauteil als integraler Einzelkörper vor.In a variant of the carrier, which is also transverse to the longitudinal extension of the upper and lower chord has increased strength, the upper and lower chords are connected by two coiled side straps connected. In addition to their stiffening function, the side straps also form a cover for the intermediate structure. This prevents foreign bodies from entering the intermediate structure and may also be desirable for aesthetic reasons. For manufacturing reasons and because of the better integration of the side straps into the overall structure, the side straps are included Advantage wrapped integrally with the top and bottom straps and the intermediate structure. To this Formed in this way, the entire load-bearing component is present as an integral individual body.
In einer Variante der Erfindung sind die Aussengurtteile kreisförmig angeordnet und bilden eine im wesentlichen ringförmige Aussenfläche. Beispielsweise ist das gewickelte Bauteil eine Felge. Die Verbundfelge weist eine ausreichend hohe Festigkeit auf. Dabei ist sie deutlich leichter als vergleichbare Felgen konventioneller Stahlbauart. Selbst gegenüber Felgen aus Aluminium weist die Verbundfelge Gewichtsvorteile auf. Die kreisförmige Anordnung der Aussengurtteile, die durch eine fachwerkartig gewickelte Zwischenstruktur miteinander verbunden sind, erlaubt auch die Herstellung anderer rotationssymmetrischer Bauteile, beispielsweise Greiferräder, die zur Fertigung von Bändern, Gurten und dergleichen eingesetzt werden. In a variant of the invention, the outer belt parts are arranged in a circle and form an inside essentially annular outer surface. For example, the wound component is a rim. The Composite rim has a sufficiently high strength. It is much lighter than comparable ones Rims of conventional steel construction. Even compared to aluminum rims, the Composite rim weight advantages. The circular arrangement of the outer belt parts through a half-timbered intermediate structure is connected to each other, also allows the production other rotationally symmetrical components, for example gripper wheels, used for manufacturing of tapes, belts and the like are used.
Dem Anwendungszweck entsprechend kann das Bauteil mit einer weitgehend geschlossen ausgebildeten Aussenhaut versehen sein, die ein Eindringen und eine Ablagerung von Verunreinigungen in das Innere des Bauteils verhindert.Depending on the application, the component can be designed to be largely closed Outer skin to be provided, the penetration and deposition of contaminants prevented inside the component.
Bei dem erfindungsgemässen Verfahren zur Herstellung eines Bauteils aus einem kunstharzimprägnierten Faserhalbzeug wird das Faserhalbzeug in einem Wickelverfahren, vorzugsweise gerichtet, auf einen Wickelkern gewickelt und danach ausgehärtet und getrocknet. Das Verfahren zeichnet sich insbesondere dadurch aus, dass bei der Wicklung des Faserhalbzeug um eine Anordnung von Wickelspulen eine Anzahl von Aussengurtteilen erstellt und wickeltechnisch integral mit einer fachwerkartig aufgebauten Zwischenstruktur gewickelt werden. Bei dem erfindungsgemässen Verfahren werden somit der Ober- und der Untergurt sowie die fachwerkartige Zwischenstruktur des gewickelten Bauteils integral, im selben Arbeitsgang aus einem quasi-unendlichen Faserhalbzeug gewickelt. Dadurch liegen die Aussengurtteile die diese verbindende Zwischenstruktur als Einzelelement vor. Die Hohlräume zwischen den Aussengurtteilen und der Zwischenstruktur werden wenigstens bereichsweise mit einem Füllmaterial gefüllt. Die konstruktive Auslegung und die Füllung der Hohlräume erhöht die Festigkeit des Bauteils insgesamt und erleichtert den Herstellungsprozess. Durch den integralen Wickelvorgang ist das Bauteil sehr einfach, den Anforderungen gemäss, ausleg- und wickelbar. Das Füllmaterial stützt die auf Druck belasteten Abschnitte der fachwerkartigen Zwischenstruktur und verhindert ein unkontrolliertes Ausknicken derselben bei Überschreitung der Belastung, für die sie ausgelegt sind.In the method according to the invention for producing a component from a synthetic resin impregnated Semi-finished fiber is the semi-finished fiber in a winding process, preferably straightened, wound on a winding core and then cured and dried. The process draws is characterized in particular by the fact that in the winding of the semi-finished fiber an arrangement of Winding spools created a number of outer belt parts and integrally with a winding technology truss-like intermediate structure can be wound. In the method according to the invention the upper and lower chord and the truss-like intermediate structure of the wound component integrally, in the same operation from a quasi-infinite semi-finished fiber wound. As a result, the outer belt parts lie the intermediate structure connecting them as a single element in front. The voids between the outer belt parts and the intermediate structure are at least partially filled with a filling material. The constructive design and the filling The cavities increase the overall strength of the component and facilitate the manufacturing process. Due to the integral winding process, the component is very simple, according to the requirements, can be laid out and wound. The filling material supports the sections of the truss-like sections that are subjected to pressure Intermediate structure and prevents an uncontrolled buckling of the same when exceeded the load for which they are designed.
Beim Einsatz des Bauteils als Träger im Fahrzeugbau kann das Füllmaterial u.a. die Energieaufnahme im Crashfall begünstigen und ein unkontrolliertes Ausknicken von auf Druck belasteten Zweigen der fachwerkartigen Zwischenstruktur verhindern. Als Füllmaterial wird beispielsweise ein technischer Kunststoffschaum gewählt, der physikalisch oder chemisch schäumbar ist. Alternativ dazu oder in Ergänzung kann auch ein Metall- oder Keramikschaum als Füllmaterial in die Zwischenräume eingebracht werden.When using the component as a carrier in vehicle construction, the filling material can include the energy intake favor in the event of a crash and an uncontrolled buckling of those under pressure Prevent branches of the truss-like intermediate structure. As a filler, for example we chose a technical plastic foam that is physically or chemically foamable. alternative in addition or in addition, a metal or ceramic foam can also be used as a filling material in the Spaces are introduced.
Eine zweckmässige Verfahrensvariante zur Herstellung von Bauteilen aus faserverstärktem Kunststoff, deren Festigkeit noch weiter verbessert ist, umfasst insbesondere die folgenden Verfahrensschritte:
- das quasi-endlose kunstharzimprägnierte Faserhalbzeug wird über Wickelspulen gewickelt, die für die Zwecke des Wickelvorgangs lösbar auf einer Wickelplatte befestigt werden;
- das gewickelte Bauteil wird in einer rahmenartigen Schliessform angeordnet, die sich auf der Wickelplatte abstützt und das Bauteil an den Längs- und Querseiten umschliesst;
- die Schliessform wird mit einem Deckel verschlossen, der mit verschliessbaren Einfüllöffnungen für das Füllmaterial, insbesondere einen physikalisch oder chemisch schäumbaren, technischen Schaum und/oder einen Metall oder Keramikschaum, versehen ist, um die in dem Bauteil verbleibenden Zwischenräume bei Bedarf wenigstens bereichsweise zu verfüllen;
- das gewickelte Bauteil wird beispielsweise durch Erhitzen des Wickelkerns derart erhitzt, dass das Füllmaterial expandiert, wobei das Bauteil verdichtet wird;
- das gewickelte Bauteil wird entfonnt wobei es vor oder gegebenenfalls nach der Entformung in
einer Tempereinrichtung getempert wird.
Durch die Verdichtung des Bauteils bei der geschilderten Verfahrensführung wird dieses hinsichtlich der Stöchiometrie optimiert, und seine Festigkeit wird noch zusätzlich erhöht.
- the quasi-endless resin-impregnated fiber semi-finished product is wound over winding spools, which are detachably fastened to a winding plate for the purposes of the winding process;
- the wound component is arranged in a frame-like closing shape, which is supported on the winding plate and encloses the component on the long and short sides;
- the closing mold is closed with a lid which is provided with closable filling openings for the filling material, in particular a physically or chemically foamable technical foam and / or a metal or ceramic foam, in order to fill the gaps remaining in the component at least in certain areas, if necessary;
- the wound component is heated, for example, by heating the winding core in such a way that the filling material expands, the component being compressed;
- the wound component is removed, and is annealed in a tempering device before or, if necessary, after removal from the mold.
By compressing the component in the process described, it is optimized in terms of stoichiometry, and its strength is further increased.
Das erfindungsgemässe Verfahren zur Herstellung von faserverstärkten Bauteilen ermöglicht es, die Anzahl der über- und/oder nebeneinander erstellten Wicklungen und den Verlauf der Wicklungen über die neben- und hintereinander angeordneten Wickelspulen in Abhängigkeit von den von dem gewickelten Bauteil aufzunehmenden Kräften zu wählen. Dadurch kann das Bauteil spezifisch für die geplante Belastung ausgelegt werden. Der konstruktive Aufbau des Bauteils nach Fachwerkträgerart ermöglicht dabei eine relativ einfache Berechnung des Bauteils und der spezifischen Auslegung.The method according to the invention for producing fiber-reinforced components makes it possible to the number of windings created one above the other and / or next to one another and the course of the windings over the coils arranged side by side and one behind the other depending on the to select the forces to be absorbed by the wound component. This allows the component to be specific be designed for the planned load. The structural design of the component according to the type of truss enables a relatively simple calculation of the component and the specific one Interpretation.
Die Wickelspulen können nach dem Wickelvorgang von dem Bauteils entfernt werden, um sie für die Herstellung weiterer Bauteil weiterzuverwenden. Es kann auch vorgesehen sein, einzelne Wikkelspulen, die als Inserts ausgebildet wurden und mit Anschlusseinrichtungen, beispielsweise Gewindebohrungen, für die Befestigung weiterer Anschlussbauteile ausgestattet wurden, derart in das gewickelten Bauteil einzubinden, dass sie einen integralen Bestandteil des Bauteils bilden.The winding coils can be removed from the component after the winding process in order for them continue to use the manufacture of additional components. It is also possible to provide individual winding coils, which were designed as inserts and with connection devices, for example threaded holes, were equipped for the attachment of further connection components, such as in the integrated component that they form an integral part of the component.
Damit die in Längsrichtung der Fasern ausgezeichnete Festigkeit des Faserhalbzeugs im Bauteil genügend zur Geltung kommt, wird das Faserhalbzeug während des Wickelprozesses im der fachwerkartigen Zwischenstruktur jeweils über wenigstens zwei nebeneinander angeordnete Wickelspulen des Wickelkerns geführt, bevor die Längsausrichtung der Fasern durch eine Änderung der Wickelrichtung geändert wird. This ensures the excellent strength of the semi-finished fiber in the component in the longitudinal direction of the fibers comes into its own, the semifinished fiber product becomes during the winding process in the framework-like Intermediate structure in each case via at least two winding coils arranged next to one another of the winding core before the longitudinal alignment of the fibers by changing the Winding direction is changed.
Für die Festigkeit des tragenden Bauteils erweist sich ein Parallelwickelverfahren von Vorteil, bei dem das Faserhalbzeug in im wesentlichen parallel zueinander verlaufenden Wicklungen über die einzelnen Wickelspulen gewickelt wird. Kreuzungen der Wicklungen kommen auf den Wickelspulen praktisch nur bei übereinanderliegenden Wicklungsschichten vor.A parallel winding process has proven to be advantageous for the strength of the load-bearing component which the semifinished fiber product in essentially parallel windings over the individual winding coils is wound. Crossings of the windings come on the winding spools practically only with superimposed winding layers.
Das erfindungsgemässe Verfahren kann von Hand, halbautomatisch oder vollautomatisiert durchgeführt werden. Insbesondere eignet sich das erfindungsgemässe Verfahren für CNCbahngesteuerte Wickelmaschinen, welche die Möglichkeit bieten, die Faserlage, das Wickelmuster, die Fadenspannung, das stöchiometrische Verhältnis von Fasern zur Kunstharzmatrix usw. mikroprozessorkontrolliert zu steuern und zu regeln. In Verbindung mit einem programmierbaren Maschinenrechner können die ermittelten Belastungswerte unmittelbar in Auslegungsdaten umgesetzt und für die Steuerung und Regelung der Wickelmaschine herangezogen werden.The method according to the invention can be carried out manually, semi-automatically or fully automatically become. The method according to the invention is particularly suitable for CNC path-controlled Winding machines, which offer the possibility of changing the fiber layer, the winding pattern, the thread tension, the stoichiometric ratio of fibers to the resin matrix, etc. microprocessor controlled to control and regulate. In connection with a programmable machine computer the determined load values can be directly converted into design data and be used for the control and regulation of the winding machine.
Als Faserhalbzeug kommen bei dem erfindungsgemässen Verfahren mit Vorteil carbonisierte Naturfasern aus Flachs, Hanf oder Chinaschilf oder Carbon-, Aramid- und/oder E-Glasrovings zur Anwendung, die vorgängig oder erst unmittelbar vor dem Wickelvorgang in einer Imprägniereinrichtung mit einer duroplastischen oder thermoplastischen Matrix eines Zwei-Komponenten-Harzes getränkt werden. Die Stärkte des imprägnierten Rovings wird zu etwa 1,5 mm bis etwa 4 mm, vorzugsweise etwa 2,5 mm, gewählt.In the process according to the invention, carbonized natural fibers are advantageously used as semi-finished products made of flax, hemp or Chinese reed or carbon, aramid and / or e-glass rovings Application that is done beforehand or just before the winding process in an impregnation device with a thermosetting or thermoplastic matrix of a two-component resin be soaked. The thickness of the impregnated roving is preferably about 1.5 mm to about 4 mm about 2.5 mm.
Das Anwendungsgebiet der erfindungsgemässen, gewickelten, tragenden Bauteile erstreckt sich vom Einsatz im Fahrzeugbau über maschinenbauliche Anwendungen, den Hoch- und Tiefbau bis zu Weltraumanwendungen. Anwendungen finden sich überall dort, wo eine Leichtbauweise erforderlich oder erwünscht ist. Als besonderes Verwendungsgebiet wird dabei der Fahrzeugbau herausgestrichen, wo der erfindungsgemässe Aufbau der Bauteile und das Herstellungverfahren eine einfache Auslegung der Bauteile für den Einsatz als Crashelemente im Chassisbau ermöglicht. Im Fall von Trägern wird das Bauteil mit einem gewickelten Ober- und einem gewickelten Untergurt hergestellt, die durch eine integral gewickelte, fachwerkartige Zwischenstruktur miteinander zu einer Einheit verbunden sind. In einer alternativen Ausführungsvariante wied wickeltechnisch eine Anzahl von Aussengurtteilen hergestellt, die kreisförmig angeordnet sein. Dabei wechseln sie am Kreisumfang mit grossen Wickelspulen ab. Das kunstharzimprägnierte Faserhalbzeug wird dabei vor und nach dem Wickeln eines Aussengurteils über jeweils eine grosse Wickelspule geführt. Zwischen dem Wickeln über zwei am Umfang angeordnete grosse Wickelspulen wird das Faserhalbzeug jeweils durch einen Abschnitt der fachwerkartigen Zwischenstruktur geführt. The field of application of the wound, load-bearing components according to the invention extends from use in vehicle construction to mechanical engineering applications, civil engineering to to space applications. Applications can be found wherever lightweight construction is required or is desired. Vehicle construction is highlighted as a special area of application, where the construction of the components according to the invention and the manufacturing process simple design of the components for use as crash elements in chassis construction. in the In the case of beams, the component is wrapped with a top and a bottom flange manufactured by an integrally wound, truss-like intermediate structure connected to a unit. In an alternative embodiment, one is used for winding Number of outer belt parts made, which are arranged in a circle. They switch on Circumference with large winding spools. The semi-finished fiber-impregnated resin is thereby before and after winding an outer belt part each over a large winding spool. The semi-finished fiber is between the winding over two large winding coils arranged on the circumference each led through a section of the truss-like intermediate structure.
Im Folgenden wird die Erfindung unter Bezugnahme auf die Figuren näher erläutert. Es zeigen in nicht massstabsgetreuer Darstellung:
- Fig. 1
- eine schematische Prinzipdarstellung des Wickelverfahrens;
- Fig. 2
- eine schematische Darstellung der Komponenten einer Wickelanlage;
- Fig. 3
- einen Grundaufbau eines Beispiels eines Wickelbauteils mit angedeutetem Wicklungsverlauf;
- Fig. 4
- eine teilweise auseinandergezogene Darstellung eines Wickelbauteils mit für die Durchführung des Herstellungsverfahrens benötigten Elementen;
- Fig. 5
- ein Ausführungsbeispiel eines entformten Bauteils; und
- Fig. 6
- ein Ausführungsbeispiel für ein rotationssymmetrisches Wickelbauteil mit angedeutetem Wicklungsverlauf.
- Fig. 1
- a schematic diagram of the winding process;
- Fig. 2
- a schematic representation of the components of a winding system;
- Fig. 3
- a basic structure of an example of a winding component with indicated winding course;
- Fig. 4
- a partially exploded view of a winding component with elements required for performing the manufacturing process;
- Fig. 5
- an embodiment of a demolded component; and
- Fig. 6
- an embodiment for a rotationally symmetrical winding component with indicated winding course.
Fig. 1 zeigt schematisch ein als Fasemasswickelverfahren bekanntes Verfahren, das bevorzugt zur
Herstellung der erfindungsgemässen Bauteile aus faserverstärktem Kunststoff zum Einsatz kommt.
Dabei wird ein von einer Spanneinheit 2 unter Vorspannung gehaltenes Faserhalbzeug P von einer
Vorratsspule 1 abgezogen und durch eine Inprägniereinheit 3 geführt. Die Imprägniereinheit 3 kann
als Tauchtränkvorrichtung oder, wie beispielsweise dargestellt, als Walzenimprägniervorrichtung
ausgebildet sein. Dem Fachmann sind die verschiedenen Formen von Imprägniereinheiten hinlänglich
bekannt, sodass auf eine nähere Erläuterung verzichtet werden kann. Das in der Imprägniereinheit
3 mit einem Kunstharzsystem imprägnierte Faserhalbzeug P wird anschliessend mittels
einer Führungseinheit 4, die mit einer rechnergesteuerten Wickelmaschine verbunden ist, auf einem
mit der Führungseinheit 4 synchronisiert rotierenden Wickelkern 5 abgelegt. Danach wird der
Wickelkörper getrocknet. Das Faserhalbzeug umfasst beispielsweise direktionierte Carbon-, Aramid-
oder Glasfasern als Einzelfasern oder, je nach Erfordernis, in beliebiger Kombination miteinander
und liegt als Roving mit einer Stärke von etwa 1,5 mm bis etwa 4 mm, vorzugsweise 2,5
mm, vor. Es können auch carbonisierte Naturfasern aus Flachs, Hanf oder Chinaschilf eingesetzt
werden. Das Kunstharz ist mit Vorteil ein thermoplastisches oder duroplastisches 2-Komponenten-Harz,Fig. 1 shows schematically a process known as bulk fiber winding method, which is preferably for
Production of the components according to the invention from fiber-reinforced plastic is used.
In this case, a semi-finished fiber P held by a
Fig. 2 zeigt ein Beispiel einer Wickelanlage 10, insbesondere einer rechnergesteuerten CNC-Wickelanlage.
Diese umfasst eine Wickelmaschine 11, einen Maschinensteuerung 12 und einen
Maschinenrechner 13. Die Wechselwirkung der einzelnen Anlagenkomponenten miteinander ist
durch die Doppelpfeile 14 und 15 verdeutlicht. Der Maschinenrechner 13 dient zur Echtzeit-Regelung
der Maschine und zur Echtzcit-Verwaltung der Steuerdaten im Steuermodus. Er erlaubt
eine Programmierung, Verwaltung und graphische Darstellung der Steuerdaten im Programmmodus.
Darüber hinaus ist es über den Maschinenrechner möglich, die Steuerdaten, beispielsweise die
Drehzahl des Wickelkerns, zu optimieren. Die Maschinensteuerung 12 der Wickelanlage 10 ist
veranwortlich für die Regelung, Steuerung und die Kommunikation. Für die Regelung des Wickelablaufs,
insbesondere der Wickelbahnachsen, wird der zeitliche Istwert-Verlauf der Achsenpositionen
laufend einem vorprogrammierten bzw. zuvor errechneten Sollwert-Verlauf angepasst. Die
Maschinensteuerung steuert bzw. regelt auch laufend weitere relevante Prozessparameter, beispielsweise
die Fadenspannung des Faserhalbzeugs. Die Kommunikationsfunktion ermöglicht einen
Datenaustausch zwischen der Wickelmaschine 11 und dem Maschinenrechner 13. Die Wikkelmaschine
10 ist bevorzugt als Drehwickelmaschine mit einer Drehachse für den Wickelkopf,
einem in der Ebene verstellbaren Schlitten und einer Zustellachse ausgebildet. Die Elemente der
Wickelmaschine besitzen die erforderliche Anzahl von Bewegungsfreiheitsgraden, damit Bauteile
der gewünschten Art wickelbar sind. Für die Herstellung etwas komplexerer Bauteile sind bevorzugt
sechs Bewegungsfreiheitsgrade vorgesehen.2 shows an example of a winding
Fig. 3 zeigt eine Ausgangssituation für die Herstellung eines erfindungsgemässen Bauteils. Dabei
ist eine Anzahl von Wickelspulen, die mit den Bezugszeichen 21 - 30 durchnumeriert sind, nebenund
hintereinander auf einer Wickelplatte 20 montiert. Die Wickelplatte 20 bildet dabei einen Bestandteil
des Wickelkerns 5 (Fig. 1). Die Wickelspulen 21 - 30 können aus Metall oder aus Kunststoff
sein. Das von der Vorratsspule als Roving abgezogene, imprägnierte Faserhalbzeug P wird
nach einem vorgegebenen Wickelplan auf die Wickelspulen 21 - 30 abgelegt. Der Wickelplan
richtet sich dabei nach den im Maschinenrechner abgelegten Steuerdaten, die vorzugsweise in Abhängigkeit
von der zu erwartenden Belastung des herzustellenden Bauteils ermittelt wurde. Ein
derartiger Wickelplan kann beispielsweise durch die Angabe der hintereinander anzufahrenden
Wickelspulen festgelegt werden. Beispielsweise könnte ein derartiger Wickelplan den folgenden
Verlauf aufweisen: S; 21; 23; 26; 28; 29; 30; 29; 30; 28; 25; 23; 22; 21; 22; 21; 24; 26; 27; 29; 30;
27; 25; 24; 22; 21; 23; 25; 27; 29; 30; 28; 26; 24; 22; 21; usw.; E. Dabei bezeichnen S den Anfang
des abgelegten Rovings P, die Bezugszeichen die in Wickelrichtung aufeinanderfolgenden Wickelspulen
und E das Ende des Rovings P. Der angegebene Wickelplan dient nur zur Erläuterung des
Wickelablaufs und stellt daher kein zwingendes Schema dar. Vielmehr ist je nach der zu erstellenden
Bauteilgeometrie jeweils ein neuer Wickelplan festzulegen. Dabei ist zu berücksichtigen, dass
für eine möglichst hohe Belastbarkeit der Roving möglichst lange direktioniert geführt wird, bevor
die Wickelrichtung und damit die Direktionierung der Fasern geändert wird.3 shows an initial situation for the production of a component according to the invention. there
is a number of winding coils, numbered 21-30, next to and below
mounted one behind the other on a winding
Fig. 4 zeigt den apparativen Aufbau für einen weiteren vorteilhaften Verfahrenschritt bei der Herstellung
eines erfindungsgemässen, tragenden Bauteils aus faserverstärktem Kunststoff. Das fertig
gewickelte Bauteil ist gesamthaft mit dem Bezugszeichen 40 versehen. In der Darstellung ist angedeutet,
dass einzelne der Wickelspulen 21 - 30 als Verlierteile ausgebildet sein können. Diese verbleiben
im gewickelten Bauteil und bilden einen integralen Bestandteil. Beispielsweise können sie
als Inserts 21, 22, 29, 30 ausgebildet sein, die mit Gewindebohrungen 35 zum Anschluss weiterer
Bauelemente an das Bauteil 40 ausgestattet sind. Die übrigen Wickelspulen 23 - 28 können vom
Bauteil 40 entnehmbar sein, um sie für die Herstellung weiterer gewickelter Bauteile weiterzuverwenden.
Das fertig gewickelte Bauteil 40 ist in Fig. 4 immer noch auf der Wickelplatte 20 angeordnet.
Für den nächsten Verfalwensschritt wird es von einer rahmenartigen Schliessform 31 umgeben,
deren Innenkontur auf die Form des Bauteils abgestimmt ist. Die Schliessform 31 stützt sich
auf der Wickelplatte 20 ab und ist durch einen Deckel 32 verschliessbar. Der Deckel ist mit Bohrungen
und verschliessbaren Einfüllöffnungen 33 versehen, durch die ein Füllmaterial in die im
gewickelten Bauteil 40 verbleibenden Hohlräume einfüllbar ist. Als Füllmaterial wird bevorzugt
ein physikalisch oder chemisch aufschäumbarer technischer Kunststoff oder ein Metall- oder Keramikschaum
eingesetzt. Durch die Expansion des Füllmaterials während des Trocknens des Bauteils
40 in der verschlossenen Schliessform 31 erfolgt eine Verdichtung der Wicklungen. Dadurch
wird die Festigkeit des gewickelten Bauteils 40 noch weiter erhöht. Nach der Verdichtung wird das
Bauteil 40 in der Schliessform oder nach seiner Entformung getempert.Fig. 4 shows the apparatus structure for a further advantageous process step in the manufacture
of a load-bearing component made of fiber-reinforced plastic according to the invention. That done
The wound component is provided with the
Fig. 5 zeigt ein Ausführungsbeispiel eines fertig gewickelten und entformten Bauteils 40. Das
Bauteil umfasst einen Obergurt 41 und einen Untergurt 42, die durch eine fachwerkartig aufgebaute
Zwischenstruktur 43 einstückig miteinander verbunden sind. An seinen Längsenden besitzt das
Bauteil 40 jeweils einen Seitengurt 44, 45 der ebenfalls integral mit den Ober- und Untergurten 41,
42 und der fachwerkartigen Zwischenstruktur 43 gewickelt ist. In die Seitengurte 44, 45 eingebunden
sind die Inserts 21, 22 bzw. 29, 30, die jeweils mit Gewindebohrungen 35 zum Anschluss weiterer
Strukturelemente ausgestattet sind. Das die Zwischenräume zwischen den Ober- und Untergurten
42, 42 und der Zwischenstruktur 43 ausfüllende, geschäumte Füllmaterial ist mit dem Bezugszeichen
46 versehen. Zur Verdeutlichung sind die geschäumten Füllkörper 46 verschieden weit
eingesetzt dargestellt. Die Wandstärken der Ober- und Untergurte 41, 42, der Seitengurte 44, 45
sowie der fachwerkartigen Zwischenstruktur 43 können je nach der zu erwartenden Belastung des
Bauteils, gemäss der berechneten Auslegung bereichsweise unterschiedlich ausgebildet sein. Dies
kann durch eine unterschiedliche Wicklungsdichte erreicht werden. Dadurch kann das Bauteil aus
faserverstärktem Kunststoff hinsichtlich seines späteren Einsatzes massgeschneidert werden. Beispielsweise
können gezielt geschwächte Bereiche eingebaut werden, um beim Einsatz des Bauteils
in einem Fahrzeugchassis eine Knautschzone zu realisieren. Als Abdeckung gegenüber Verschmutzungen
kann das Bauteil 40 noch mit einer Aussenhaut, beispielsweise einer aufgespritzten
Kunststoffhaut versehen sein. Um den Einsatz in extrem widrigen Umwelteinflüssen physischen
oder chemischen Ursprungs zu gewährleisten, kann die gewickelte Tragstruktur herkömmlich umspritzt
werden. Dadurch lassen sich auf einfachste Weise Oberflächenschutz und A Klasse Oberflächenqualität
vereinen.5 shows an exemplary embodiment of a completely wound and
Das in Fig. 6 angedeutete Wickelbauteil ist im wesentlichen rotationssymmetrisch aufgebaut und
trägt gesamthaft das Bezugszeichen 50. Dabei zeigt die Darstellung ein ringförmig angeordnetes
Profil, bei dem am Umfang angeordnete grosse Wickelspulen 57 - 61 mit Aussengurtteilen 62 - 66
abwechseln. Die Aussengurtteile 62 - 66 sind dabei vorzugsweise auf kreissegmentartig gekrümmte
Aussenformteile gewickelt. Die fachwerkartige Zwischenstruktur weist Wickelspulen 51 - 56 auf.
Der Wickelablauf kann beispielsweise den folgenden Verlauf aufweisen: von der im Zentrum befindlichen
Wickelspule 51 wird das Faserhalbzeug P, beispielsweise ein imprägnierte Gewebeband,
zur Wickelspule 52 und von dort auf die am Umfang befindliche grosse Wickelspule 57 geführt.
Die grosse Wickelspule 57 wird vorzugsweise umwickelt bevor das Gewebeband P zu dem kreissegmentartig
gekrümmten Aussenformteil zur Bildung des Aussengurtteils 62 geleitet wird, um
dieses gewickelt und zur nächsten grossen Wickelspule 61 geführt wird. Im Anschluss an die grosse
Wickelspule 61 wird das Gewebeband P wieder in die fachwerkartige Zwischenstruktur geführt,
wo es zunächst unidirektional über die Wickelspulen 56 und 51 geführt wird, bevor seine
Wickelrichtung in Richtung auf die Wickelspule 54 geändert wird. Von der Wickelspule 54 gelangt
das Gewebeband P zu am Umfang angeordenten grossen Wickelspule 59. Diese wird vorzugsweise
wenigstens einmal umrundet, bevor das Gewebeband P auf das Aussenformteil für das Aussengurtteil
64 geleitet wird. Im Anschluss an das Aussengurtteil 64 wird das Gebebeband P um die
benachbarte grosse Wickelspule 58 geführt, bevor es wieder zu den Wickelspulen in der fachwerkartigen
Zwischenstruktur geleitet wird, usw. Auf diese Weise ist sichergestellt, dass das Gewebeband
immer abwechselnd über einen Abschnitt des Umfangs und die Zwischenstruktur geführt
wird. Am Umfang wird das Gewebeband P immer über zwei grosse Wickelspulen und ein dazwischen
angeordnetes Aussengurtteil geführt. In der Zwischenstruktur wird das Gewebeband immer
zunächst über zwei benachbarte Wickelspulen geführt bevor seine Wickelrichtung ändert. Zusammengefasst
ergibt sich daraus beispielsweise die folgende Wickelabfolge: 51-52-57 62-61-56-51-54-59-64-58,53-51-56-61-63-60-55-51-53-58-66-57-52-51-55-60-64-59-54-51-usw.
Als Gewebeband
kommen neben Rovings mit direktionierten Fasern auch gewobene, geflochtene, gestrickte
oder in einer anderern Art vernetzte Fäden, aber auch wirre Fliessbänder zur Anwendung.The winding component indicated in FIG. 6 is essentially rotationally symmetrical and
bears the
Claims (29)
- A component of fiber-reinforced plastic, in which a synthetic-resin-impregnated semi-finished fiber product (P) is wound, preferably in multiple layers, with preferably directional fibers about a winding core (5), characterized in that the component (40; 50) is embodied as a load-bearing element and includes wound outer belt elements, which are joined to one another via an intermediate structure wound in trelliswork-like fashion, the voids between the outer belt elements (41, 42) and the intermediate structure (43) being filled at least in some regions with a filler material (46).
- The component of claim 1, characterized in that the filler material (46) is a physically or chemically foamable plastic or a metal or ceramic foam.
- The component of claim 2, characterized in that the wound component (40), filled with a foamable filler material, is compacted.
- The component of one of the foregoing claims, characterized in that the outer belt elements (41, 42) and the trelliswork-like intermediate structure (43) are wound integrally from a quasi-endless semi-finished fiber product (P).
- The component of one of the foregoing claims, characterized in that the semi-finished fiber product (P) includes a synthetic-resin-impregnated roving approximately 1.5 mm to approximately 4 mm and preferably approximately 2.5 mm thick.
- The component of one of the foregoing claims, characterized in that the semi-finished fiber product (P) includes a combination of different kinds of fiber structures, with preferably identically oriented fibers.
- The component of one of the foregoing claims, characterized in that the synthetic resin used for the impregnation is pressure-setting or thermoplastic.
- The component of one of the foregoing claims, characterized in that the winding core (5) includes a number of winding spools (21, 30), which for the winding process are mounted detachably on a winding plate (20).
- The component of claim 8, characterized in that individual ones of the winding spools (21, 22, 29, 30) are embodied as inserts with connection devices (35), for instance threaded bores, for further connection components.
- The component of claim 8 or 6, characterized in that the plastic-impregnated semi-finished fiber product (P), in the region of the trellis work-like intermediate structure, is guided over at least two adjacent winding spools before it changes its winding direction.
- The component of one of the foregoing claims, characterized in that the synthetic-resin-impregnated semi- finished fiber product (P) is in the form of essentially parallel-extending strips wound side by side and/or one over the other.
- The component of one of the foregoing claims, characterized in that regions of the outer belt elements (41, 42) and of the trelliswork-like intermediate structure (43) have a requirement-specific different number of windings.
- The component of one of the foregoing claims, characterized in that the outer belt elements include a wound upper and lower belt (41, 42), which are joined to one another by the trelliswork-like intermediate structure (43).
- The component of claim 13, characterized in that the upper and lower belt (41, 42) are joined to one another by two wound side belts (44, 45).
- The component of claim 14, characterized in that the side belts (44, 45) are wound integrally with the upper and lower belt (41, 42) and the intermediate structure (43).
- The component of one of claims 1-12, characterized in that the outer belt elements (62, 66) are disposed in circular form and form a substantially annular outer surface of a substantially rotationally symmetrical object (50).
- The component of one of the foregoing claims, characterized in that it is provided with an outer skin embodied in substantially closed fashion.
- A method for producing a component (40) from a synthetic-resin-impregnated semi-finished fiber product (P), in which the semi-finished fiber product (P) is wound, preferably in oriented fashion, in a winding process onto a winding core (5) and then hardened and dried, characterized in that the semi-finished fiber product (P) is wound around an arrangement of winding spools (21, 30), and outer belt elements are made and wound integrally in terms of winding technique with an intermediate structure (43) embodied in trelliswork-like fashion, and the voids between the outer belt elements (41, 42) and the intermediate structure (43) are filled at least in some regions with a filler material (46).
- The method of claim 18, characterized in that the interstices between the outer belt elements (41, 42) and the intermediate structure (43) are filled at least in some regions with a filler material (46), preferably being foamed with a technical plastic foam or a metal or ceramic foam.
- The method of claim 19, characterized in that the synthetic-resin-impregnated semi-finished fiber product (P) is wound over winding spools (21-30), which for the purposes of the winding operation are secured detachably to a winding plate (20); that the wound component (40) is disposed in a framelike closing form (31) which is braced on the winding plate (20) and encloses the component (40); that the closing form (31) is closed with a cap (32), and the cap (32) is provided with closable fill openings (33) for the filler material (46), in particular a physically or chemically foamable technical foam, in order at least in some regions, as needed, to fill the interstices remaining in the component (40); that the wound component (40) is heated, for instance by heating the winding core, in such a way that the filler material expands, and the component is compacted before being unmolded; and that the wound component (40) is tempered in a tempering device before or optionally after the unmolding.
- The method of one of claims 18-20, characterized in that the number of windings made one over the other and/or side by side and the course of the windings along the winding spools (21-30) disposed side by side and one after the other is selected as a function of the forces to be absorbed by the wound component (40).
- The method of one of claims 18-21, characterized in that individual ones of the winding spools (21, 22, 29, 30) are selected as inserts, which are equipped with connection devices (35), such as threaded bores, for securing further connection components.
- The method of claims 20-22, characterized in that the semi-finished fiber product (P) in the trelliswork-like intermediate structure is guided in each case over at least two winding spools, disposed side by side, of the winding core, before the longitudinal orientation of the fibers is changed by changing the winding direction.
- The method of one of claims 20-23, characterized in that the semi-finished fiber product (P) is wound in essentially parallel-extending windings over a winding spool.
- The method of one of claims 18-24, characterized in that the winding process is performed in automated fashion.
- The method of one of claims 18-25, characterized in that as the semi-finished fiber product, carbonized natural fibers of flax, hemp or Chinese reed or carbon, aramide and/or elastic glass rovings, saturated with a pressure-setting or thermoplastic matrix of a two-component resin in a thickness of approximately 1.5 mm to approximately 4 mm, preferably approximately 2.5 mm, are used.
- The method of one of claims 18-26, characterized in that one upper belt and one lower belt (41, 42) are made and wound by winding technology integrally with the intermediate structure (43) constructed in trelliswork-like fashion.
- The method of one of claims 18-26, characterized in that by winding technology, a number of outer belt elements (62-66) is produced, which are disposed in a circle and disposed in alternation along the circumference of the circle with large winding spools (57-61), and the synthetic- resin-impregnated semi-finished fiber product (P), before and after the winding of an outer belt element, is guided in each case over a large winding spool, and between the winding, in each case one portion of the trelliswork-like intermediate structure (51-56) is wound over two large winding spools disposed on the circumference.
- The use of a load-bearing component (40; 50) of one of claims 1-17 as a bearer and/or reinforcing element for vehicles, such as passenger cars or trucks of lightweight construction, or as a carrier wheel, wheel rim, or the like.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH4132000 | 2000-03-03 | ||
| CH4132000 | 2000-03-03 | ||
| CH413002000 | 2000-03-03 | ||
| PCT/CH2001/000077 WO2001064426A1 (en) | 2000-03-03 | 2001-02-05 | Component consisting of a fibre-reinforced synthetic material and a method for producing same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1268164A1 EP1268164A1 (en) | 2003-01-02 |
| EP1268164B1 true EP1268164B1 (en) | 2003-08-13 |
Family
ID=4514491
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP01955094A Expired - Lifetime EP1268164B1 (en) | 2000-03-03 | 2001-02-05 | Component consisting of a fibre-reinforced synthetic material and a method for producing same |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US7090737B2 (en) |
| EP (1) | EP1268164B1 (en) |
| AT (1) | ATE246991T1 (en) |
| AU (1) | AU2001228248A1 (en) |
| CA (1) | CA2401028C (en) |
| DE (1) | DE50100504D1 (en) |
| WO (1) | WO2001064426A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7410687B2 (en) | 2004-06-08 | 2008-08-12 | Trex Co Inc | Variegated composites and related methods of manufacture |
| DE102007028762A1 (en) | 2007-06-22 | 2008-12-24 | Audi Ag | Bumper bracket unit for motor vehicle, has reinforcing structure and tension or compression chord formed as separately prefabricated semi-finished units |
| DE102013014032A1 (en) | 2013-06-20 | 2014-12-24 | Thyssenkrupp Presta Ag | Component made of fiber composite material and method for its production |
| DE102014019080A1 (en) | 2014-12-18 | 2015-07-02 | Daimler Ag | Process for producing a fiber-reinforced structural component |
| EP4321330A1 (en) | 2022-08-09 | 2024-02-14 | Universität Stuttgart | Method for producing coreless fibre composite components and winding pin for a fibre composite component |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2320944A1 (en) * | 2005-12-02 | 2009-05-29 | Fpk, S.A. | Composite part reinforced with a fibre part by means of diverse winding processes or direct application processes of unidirectional fibre filaments, and its methods of manufacture |
| EP1849588B1 (en) * | 2006-04-27 | 2011-06-01 | AKsys GmbH | Method of manufacture of a composite part |
| US8118958B2 (en) * | 2006-04-28 | 2012-02-21 | Moog Inc. | Composite ring gear with metallic gear insert, and method of forming same |
| ES2579228T3 (en) * | 2008-07-25 | 2016-08-08 | Sika Technology Ag | Interconnected foam or adhesive layers |
| CN102191627B (en) * | 2010-03-16 | 2013-08-07 | 机械科学研究总院先进制造技术研究中心 | Composite material three dimensional weaving equipment |
| DE102010025940A1 (en) * | 2010-07-02 | 2012-01-05 | Weberit-Werke Dräbing Gmbh | Process for producing a reinforcing structure |
| DE102010052737B3 (en) * | 2010-11-26 | 2012-04-19 | Daimler Ag | Modular manufacturing apparatus for integral semi-finished fiber products and process for the production of continuous fiber composite components from integral fiber composite semi-finished products with a hollow body structure |
| DE102017001323A1 (en) | 2017-02-11 | 2017-08-17 | Daimler Ag | Semi-finished product, in particular for the production of a vehicle, and method for producing such a semifinished product |
| FR3067279B1 (en) * | 2017-06-13 | 2021-02-19 | Conseil & Technique | PROCESS FOR MAKING A PART IN COMPOSITE MATERIAL, AND COMPOSITE PART OBTAINED |
| US10603852B2 (en) * | 2017-08-30 | 2020-03-31 | Twdt Precision Co., Ltd | Method for making bicycle crank arm |
| FR3096063A1 (en) * | 2019-05-15 | 2020-11-20 | Conseil Et Technique | Composite material construction element |
| CN115056511B (en) * | 2022-05-20 | 2024-02-13 | 中国兵器科学研究院宁波分院 | Casting device for oriented wire reinforced composite material |
| CN114953518A (en) * | 2022-06-02 | 2022-08-30 | 贵州翰凯斯智能技术有限公司 | Automobile chassis and processing method thereof |
| CN114905768A (en) * | 2022-06-02 | 2022-08-16 | 贵州翰凯斯智能技术有限公司 | A kind of processing method of automobile leaf spring |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1933228A1 (en) * | 1969-07-01 | 1971-01-21 | Trw Inc | One piece filament wound ball bearing cage |
| DE2711551C2 (en) * | 1977-03-17 | 1983-11-17 | Chas. A. Blatchford & Sons Ltd., Basingstoke, Hampshire | Load-bearing part of a leg or arm prosthesis and process for its manufacture |
| GB2004835B (en) * | 1977-09-22 | 1982-08-18 | Math F C | Cobweb structure |
| IE48838B1 (en) * | 1978-09-22 | 1985-05-29 | British Petroleum Co | Reinforced structures,their application and method of forming such structural units |
| GB2049613B (en) * | 1979-05-04 | 1983-09-01 | British Petroleum Co | Structures |
| DE3003666A1 (en) * | 1980-02-01 | 1981-08-06 | Richard 4937 Lage Pott | Mechanically laying reinforcements for laminated components - using machine which winds unidirectional layers of filaments for subsequent bonding and cure |
| US4376669A (en) * | 1980-08-15 | 1983-03-15 | The British Petroleum Company Limited | Method of fabricating energy absorbing structure |
| JPS60234762A (en) * | 1984-05-03 | 1985-11-21 | Toyoda Autom Loom Works Ltd | Method and device for producing fiber reinforced molding |
| US4629644A (en) * | 1985-09-30 | 1986-12-16 | United Technologies Corporation | Filament wound structure having filament wound reinforcing rings for use as a torque drive |
| GB2246111B (en) * | 1990-07-13 | 1994-05-04 | Samsung Heavy Ind | Dipper stick for excavator of high strength polymeric composite materials and method for manufacturing such |
| CA2136190C (en) * | 1992-09-14 | 1998-08-04 | John Kenton Britten | Structural and other components, method of manufacture |
| US5435869A (en) * | 1993-08-27 | 1995-07-25 | Christensen; Roland | Method for manufacturing a composite crank arm |
| US5632940A (en) * | 1994-03-29 | 1997-05-27 | Whatley; Bradford L. | Method of making an integrally stiffened article |
-
2001
- 2001-02-05 DE DE50100504T patent/DE50100504D1/en not_active Expired - Lifetime
- 2001-02-05 WO PCT/CH2001/000077 patent/WO2001064426A1/en not_active Ceased
- 2001-02-05 EP EP01955094A patent/EP1268164B1/en not_active Expired - Lifetime
- 2001-02-05 AU AU2001228248A patent/AU2001228248A1/en not_active Abandoned
- 2001-02-05 AT AT01955094T patent/ATE246991T1/en active
- 2001-02-05 CA CA002401028A patent/CA2401028C/en not_active Expired - Fee Related
-
2002
- 2002-08-30 US US10/231,238 patent/US7090737B2/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7410687B2 (en) | 2004-06-08 | 2008-08-12 | Trex Co Inc | Variegated composites and related methods of manufacture |
| DE102007028762A1 (en) | 2007-06-22 | 2008-12-24 | Audi Ag | Bumper bracket unit for motor vehicle, has reinforcing structure and tension or compression chord formed as separately prefabricated semi-finished units |
| DE102007028762B4 (en) * | 2007-06-22 | 2015-10-22 | Audi Ag | Biegeträgerteil for a motor vehicle and method for its production |
| DE102013014032A1 (en) | 2013-06-20 | 2014-12-24 | Thyssenkrupp Presta Ag | Component made of fiber composite material and method for its production |
| WO2014202247A1 (en) | 2013-06-20 | 2014-12-24 | Thyssenkrupp Presta Ag | Steering column for a motor vehicle and method for producing a steering column |
| US9676149B2 (en) | 2013-06-20 | 2017-06-13 | Thyssenkrupp Presta Ag | Steering columns for a motor vehicle and methods for manufacturing same |
| US9802367B2 (en) | 2013-06-20 | 2017-10-31 | Thyssenkrupp Presta Ag | Component made of a fiber composite material and process for producing same |
| DE102014019080A1 (en) | 2014-12-18 | 2015-07-02 | Daimler Ag | Process for producing a fiber-reinforced structural component |
| EP4321330A1 (en) | 2022-08-09 | 2024-02-14 | Universität Stuttgart | Method for producing coreless fibre composite components and winding pin for a fibre composite component |
| DE102022120073A1 (en) | 2022-08-09 | 2024-02-15 | Hochschule Aalen, Körperschaft des öffentlichen Rechts | Method for producing coreless fiber composite components and winding pin for a fiber composite component |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1268164A1 (en) | 2003-01-02 |
| WO2001064426A1 (en) | 2001-09-07 |
| AU2001228248A1 (en) | 2001-09-12 |
| US7090737B2 (en) | 2006-08-15 |
| DE50100504D1 (en) | 2003-09-18 |
| US20030010424A1 (en) | 2003-01-16 |
| CA2401028A1 (en) | 2001-09-07 |
| CA2401028C (en) | 2006-10-31 |
| ATE246991T1 (en) | 2003-08-15 |
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